Aerothermal study of high-pressure turbine rotor tips and casing at engine representative conditions with high-speed rotation
<p>Modern aircraft engines operate at high turbine entry temperatures to increase the cycle efficiency. The combustors employ intricate cooling techniques, to survive such high temperatures, resulting in distorted temperature profiles at the combustor exit. Further, extensive platform cooling,...
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| フォーマット: | 学位論文 |
| 言語: | English |
| 出版事項: |
2022
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